飛機構架結構 的英文怎麼說

中文拼音 [fēijīgòujiàjiēgòu]
飛機構架結構 英文
airframe construction
  • 飛 : Ⅰ動詞1 （鳥、蟲等在空中活動） fly; flit 2 （利用動力機械在空中行動） fly 3 （在空中飄浮遊動） fly...
  • 機 : machineengine
  • 構 : Ⅰ動詞1 （構造; 組合） construct; form; compose 2 （結成） fabricate; make up 3 （建造; 架屋） bui...
  • 架 : Ⅰ名詞1 （用來放置東西或支撐物體等的東西; 架子） frame; rack; shelf; stand 2 （毆打; 爭吵） fight;...
  • 結 : 結動詞（長出果實或種子） bear （fruit）; form （seed）
  • 飛機 : airplane; plane; aeroplane; kite; bird; aircraft
  • 構架 : carcass; panel work; frame; buck; blind; reinforcement; thripple; backbone; framework; truss; fra...
  • 結構 : 1 （各組成部分的搭配形式） structure; composition; construction; formation; constitution; fabric;...
  1. Joined - wing configuration features diamond - shapes in both the plan and front views. the front wing is aft swept with positive - dihedral angle and the rear wing is forward swept with negative dihedral angle

    聯結翼飛機是指帶上反角的后掠前翼和帶下反角的前掠后翼聯結成菱形框架結構的飛機。
  2. In order to affirm that our ideal and project of lab ' s establishment are right, we then introduce an example about lab ' s establishment, which is about remote real - time health monitoring system for structure of an aeromodelling ' s wing

    為了驗證我們建立實驗室的框架和方案是行得通的，文章接著又研究了採用一架航模飛機作為研究對象，來建立一套監控航模飛機機翼結構的健康監控系統。
  3. It supports the aircraft during parking and endures the loads during ground maneuvers. most of the vertical and horizontal kinetic energy are absorbed and dissipated by landing gear. it plays an extreme important role in preventing the airframe from vibration and excessive impact forces, improving passenger comfortable characteristics and increasing aircraft flight safety

    飛機起落架作為飛機結構的一個重要部件，承受著飛機與地面接觸時產生的靜、動載荷，吸收和消耗飛機在著陸撞擊、跑道滑行等地面運動時所產生的能量，在減緩飛機發生振動，降低飛機地面載荷，提高乘員舒適性，保障飛機飛行安全等方面發揮著極其重要的作用。
  4. A large planar microphone array, which consists of 111 microphones, was successfully applied to obtain a two - dimensional mapping of the sound sources on a landing aircraft. the focus of study in this paper is on the landing gear noise source. the spectra, directivities and sound pressure levels of flap side - edge noise of 7 narrow - board commercial aircraft and 7 wide - board commercial aircraft are presented. it is found that the landing gear noise spectrum is broadband with some single tones in some cases. the directivity of the total sound pressure level of a landing gear noise resembles that of a horizontal dipole. the level differences between the various aircraft landing gears are larger than those expected from the airspeed differences. it is thus expected that the louder noise emission of the landing gears can be reduced by redesigning

    應用由111個傳聲器組成的平面傳聲器陣列對當前流行的民用客機進場著陸過程中的機體噪聲源進行了實驗測量，本文對七架窄體客機和七架寬體客機的起落架噪聲進行了分析，得到了起落架噪聲的頻譜特性、指向特性和聲級變化.研究發現，起落架噪聲的頻譜是由寬頻隨機噪聲與一些較為明顯的單音噪聲源組成，起落架噪聲的指向性類似於一個水平放置的偶極子.不同飛機起落架噪聲的聲級相差較大，這說明可以通過重新結構設計降低起落架噪聲。
  5. Abstract : problems existed in using combined jig to assemble airplane are analyzed and the principle of how to select integral structure configuration of jig for airplane assembly is introduced. correct setting of three supporting points of the integral jig is discussed in the paper as well

    文摘:分析歸納了飛機裝配中採用組合式型架存在的問題；介紹了飛機裝配中型架總體結構形式的選擇原則；討論了整體式型架3個支承點應如何正確設置。
  6. Integral panel is a flat part integrated with framework elements, connection elements and skin in traditional aircraft structure, it is the main supporting structure in aircraft, having the advantages of high - intensity, low - weight, and so on

    整體壁板是將傳統飛機結構中的骨架元素、連接元素和蒙皮製成一體的板類零件，是飛機的主要受力結構件，具有強度高、重量輕、氣密性好等優點。
  7. The method is demonstrated by using real data of airplane. the airplane isar image is evidently enhanced, and the physics - based feartures of scattering centers is gained by the method

    依此框架完成了對飛機目標isar圖像有效的增強處理，提取到了反映成像目標結構特徵的點散射中心集合。
  8. Abstract : a large planar microphone array, which consists of 111 microphones, was successfully applied to obtain a two - dimensional mapping of the sound sources on a landing aircraft. the focus of study in this paper is on the landing gear noise source. the spectra, directivities and sound pressure levels of flap side - edge noise of 7 narrow - board commercial aircraft and 7 wide - board commercial aircraft are presented. it is found that the landing gear noise spectrum is broadband with some single tones in some cases. the directivity of the total sound pressure level of a landing gear noise resembles that of a horizontal dipole. the level differences between the various aircraft landing gears are larger than those expected from the airspeed differences. it is thus expected that the louder noise emission of the landing gears can be reduced by redesigning

    文摘:應用由111個傳聲器組成的平面傳聲器陣列對當前流行的民用客機進場著陸過程中的機體噪聲源進行了實驗測量，本文對七架窄體客機和七架寬體客機的起落架噪聲進行了分析，得到了起落架噪聲的頻譜特性、指向特性和聲級變化.研究發現，起落架噪聲的頻譜是由寬頻隨機噪聲與一些較為明顯的單音噪聲源組成，起落架噪聲的指向性類似於一個水平放置的偶極子.不同飛機起落架噪聲的聲級相差較大，這說明可以通過重新結構設計降低起落架噪聲。
  9. The landing impact has been recognized as a significant factor in structural fatigue damage, dynamic stress on the aircraft airframe, and crew and passenger discomfort

    而這種沖擊載荷被認為是造成飛機及其起落架結構發生疲勞與振動破壞、引起乘員不舒適的重要因素。
  10. Landing gear is one of the important equipments in the aircraft structure, it can influence the aircraft during the process of takeoff, landing and taxiing

    起落架是飛機結構中的重要裝置之一，它影響到飛機的起飛、著陸和滑跑過程。
  11. The thesis describes the conception of the object - oriented modeling and integrated simulaton enviroment, and discusses the below topics : ( 1 ) describe the reasonable structure of the modern fighter simulation system, and design the data transfer interface. ( 2 ) discuss the modeling method of the key subsystem of future fighter system especially the aerodynamics and the control system in detail. ( 3 ) construct the 3d model of the aircraft and scene, and verify the graphic simulation technique based on pc

    本文詳細討論了面向對象建模方法以及一體化模擬環境的基本概念框架及基本結構並在此基礎上提出了合理的現代戰斗機模擬系統結構，設計了模擬系統的數據傳遞介面；詳細討論了現代戰斗機模擬系統關鍵子系統? ?飛機本體、飛行控制系統建模方法；建立了用於研究的飛機以及視景的三維顯示平臺；並在此基礎上實現了實驗性的基於pc的現代戰斗機圖形模擬平臺，對模擬模型有效性確認和驗證工作做了初步的探討，研究比較了傳統飛行動力學和運動學方程和四元數法在飛行模擬中的效果。
  12. For example, with regard to part of the question about the fire resistance standard, to what degrees in temperature can our buildings withstand the extreme heat of burning, or how high the temperature of scorching heat will amount to the effect of 10 aeroplanes crashing into a building, or insofar as the fire resistant structures of our buildings are concerned, how many bomb - filled vehicles will have to crash into the base of a building for it to collapse

    主席，局長可否以量化的方式，更生動地讓我們了解有關的情況？例如就第二部分有關耐火標準的質詢而言，樓宇可以抵受多少度的高溫燃燒，或多少度的高溫燃燒會相等於受10架飛機撞擊的效果，或以我們的大廈的耐火結構計算，多少架充滿炸彈的汽車撞擊大廈底部，大廈才會倒塌呢？
  13. It is mainly made up of lognitudinal framework, latitudinal framework, airfoil shell, tie - in etc. for the frp airfoil shell, we generally use moulding method of handcraft laying

    飛機機翼曲面是一個結構復雜的非回轉曲面，其整體結構主要由縱向骨架、橫向骨架、蒙皮和接頭等構件組成。
  14. The worlds premier clean vehicle event, challenge bibendum, will make its debut in asia in october, 2004 in shanghai, china. organized by michelin, the worlds tire technology leader, the event promotes progress in the development of environmentally friendly vehicles and is an increasingly popular platform for car manufacturers to demonstrate state - of - the - art technologies in this field

    此次安凱客車帶來了兩款世界極品豪華客車， hff6120k35和hff6120wk62 ，它們是同為賽特拉家族系列成員的k35 ，安凱客車是國內唯一一家全部客車系列採用"全承載"的企業，全承載客車也稱無底盤客車，採用的是飛機製造技術的整體化框架結構技術。
  15. According as the actual conditions of one plane repair factory, the paper analyses the existing problem and style of the aircraft maintenance management in this factory, discusses the necessity of standardized aircraft maintenance management, and has put forward the framework thought of ammis based on web

    結合某飛機修理廠的實際情況，分析了該廠飛機維修流程管理存在的問題，討論了規范化飛機維修流程管理的必要性，提出了基於web的飛機維修管理信息系統的架構思想。
  16. Adopting ancillary plate structure, flywheel runs smoothly, greatly reducing the overweight during running

    J93 - 1000c機架的安全性可靠性大大提高，飛輪採用副板結構飛輪運轉過程中偏重大大降低，飛輪運轉平穩。
  17. The paper drew the conclusion of the mode of deformation and the value of internal force and the distribution of plastic zone after processing the data

    在國外，張拉整體桁架結構更是以其無法替代的優勢而被大量應用於飛機維修庫房。
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